Powder removal floating structures

ABSTRACT

An article of manufacture includes a part structure formed via a first additive manufacturing process and a floating structure within the part structure which is mechanically decoupled from the part structure. The floating structure is formed concurrently with the part structure via the first additive manufacturing process.

BACKGROUND

The present disclosure relates generally to powder removal methods andsystems for manufacturing.

Additive manufacturing or three-dimensional (3-d) printing is a processof forming an article one layer at a time. Several modalities or methodsof additive manufacturing utilize a powder-bed printing process where alayer of powder is deposited and a roller or scraper is used to levelthe height of the powder. A sourced of heat may be introduced to thepowder selectively to melt or fuse the powder. Alternatively, a bindermay be selectively applied to the powder after the powder is leveled.The process is repeated until the geometry of a part or component isprinted.

When the part is embedded in the powder bed during printing, many or allinternal structures may be filled with powder, which may be metallicand/or other materials. Post-process steps such as heat treat, surfacefinishing and subtractive manufacturing processes are often performed tofurther enhance the properties or geometry of the part. While the partis still being manufacturing, it is in a “green” state. The green partmay be less robust than a fully finished part, and special techniquesmay be required to de-powder the green part such that the part itselfdoes not break during handling and de-powdering, especially for partswith complex internal geometries and cavities.

SUMMARY OF THE INVENTION

In one aspect, an article of manufacture includes a part structureformed via a first additive manufacturing process and a floatingstructure within the part structure and mechanically decoupled from thepart structure. The floating structure is formed concurrently with thepart structure via the first additive manufacturing process.

In another embodiment a powder removal method includes identifying apart geometry, identifying a cavity within the part to place a powderremoval feature, defining at least one characteristic of the powderremoval feature, creating a build file for forming the part and thepowder removal feature via a generative build process, generativelyforming the part and the powder removal feature, and vibrating the partand the powder removal feature.

BRIEF DESCRIPTION OF THE DRAWINGS

These and other features, aspects, and advantages of the presentdisclosure will become better understood when the following detaileddescription is read with reference to the accompanying drawings in whichlike characters represent like parts throughout the drawings, wherein:

FIG. 1 is an illustration of a powder-filled part formed via additivemanufacturing;

FIG. 2 is an illustration of a part formed via additive manufacturing,including powder removal features;

FIG. 3 is an illustration of a part formed via additive manufacturing,including powder removal features;

FIG. 4 is an enlarged cross-section of a channel of a part formed viaadditive manufacturing, including a powder removal feature;

FIG. 5 is an enlarged cross-section of a channel of a part formed viaadditive manufacturing, including a powder removal feature;

FIG. 6 is an enlarged cross-section of a channel of a part formed viaadditive manufacturing, including multiple powder removal features; and

FIG. 7 is a powder removal method, according to the present embodiments.

Unless otherwise indicated, the drawings provided herein are meant toillustrate features of embodiments. These features are believed to beapplicable in a wide variety of systems comprising one or moreembodiments of the disclosure. As such, the drawings are not meant toinclude all conventional features known by those of ordinary skill inthe art to be required for the practice of the embodiments disclosedherein.

DETAILED DESCRIPTION

In the following specification and the claims, reference will be made toa number of terms, which shall be defined to have the followingmeanings.

The singular forms “a”, “an”, and “the” include plural references unlessthe context clearly dictates otherwise.

“Optional” or “optionally” means that the subsequently described eventor circumstance may or may not occur, and that the description includesinstances where the event occurs and instances where it does not.

Approximating language, as used herein throughout the specification andclaims, may be applied to modify any quantitative representation thatcould permissibly vary without resulting in a change in the basicfunction to which it is related. Accordingly, a value modified by a termor terms, such as “about”, “approximately”, and “substantially”, are notto be limited to the precise value specified. In at least someinstances, the approximating language may correspond to the precision ofan instrument for measuring the value. Here and throughout thespecification and claims, range limitations may be combined and/orinterchanged. Such ranges are identified and include all the sub-rangescontained therein unless context or language indicates otherwise.

As used herein, the term “monolithic” describes structures formed of asingle, continuous, homogeneous consistency.

As used herein, the term “modality” refers to any additive manufacturingbuild methods and processing including but not limited to binderjetting, directed energy deposition, material extrusion, selective lasermelting (SLM), material jetting, powder bed fusion, sheet lamination,welding, brazing, vat photopolymerization, stereolithography (SLA),direct metal laser melting (DMLM), fused deposition modeling (FDM),direct metal laser sintering (DMLS), and electron beam melting (EBM).There are also additive modalities that do not utilize powder. Additivemanufacturing is also referred to as a generative build process.

As used herein, the term “powder” may to various materials including butnot limited to metallic, ceramic and polymer powders. Powdercharacteristics such as size, material, density and other properties maydepend on the modality being employed.

As used herein, the terms “de-powder” and “powder removal” refer to theprocess of removing excess powder from a part following or during thebuild phase.

Among the additive manufacturing build methods that employ powder bedmodalities and/or powder as an input material, there are variations inpowder size distribution leading to varying packing density of thepowder. For example, for many modalities, a higher powder packingdensity is desired in order to decrease the porosity of the resultingfinished part. For other modalities, lower powder packing densities aredesired in order to increase the flowability of the powder which mayenhance the resolution of the fine feature details of the process. Assuch, powder removal may be more challenging in some additive modalitiesthan for others, especially modalities for which powder removal occurswhile the part is in a green state, because of limitations in theability to shake or vibrate the green part without damaging it.

FIG. 1 is an illustration of a part 10 made via additive manufacturing.The part may be in a green state, and not fully finished. The part 10includes a plurality of horizontally and vertically spaced channels 14defined between a plurality of vertical walls 16 and a plurality ofhorizontal walls 18. The part 10 may include at least one side wall 20,a top surface 22 and a bottom surface 24. Each channel of the pluralityof horizontally and vertically spaced channels 14 is filled with powder12 as a result of manufacturing via a powder bed additive manufacturingprocess. The plurality of horizontally and vertically spaced channels 14appear with rectangular and/or square cross-sections in the embodimentof FIG. 1. However, channels with other cross-sectional shapes such ascircles, triangles, parallelograms and other shapes are also possible.In addition, cavities other than channels such as voids, reservoirs,plenums, lattice structure voids, ducts, manifolds, etc. are alsopossible.

FIG. 2 is a cross-section illustration of a part 10 according to thepresent embodiments, including a top surface 22, at least one side wall20 as well as cut surfaces 26 that illustrate the plane through which acut was taken, thereby illustrating the internal details of the part 10.The cut surfaces 26 provide ease of illustration and would likely not beincluded in a part 10. The part 10 includes a plurality of verticalwalls 16 and a plurality of horizontal walls 18 which define thehorizontally and vertically spaced channels 14. Each of the channels 14is filled with powder 12 as well as at least one floating structure 28which may be formed during the build process and rests in the powder 12.In one embodiment, at least one floating structure is formedconcurrently with the part 10 or green state part structure via the sameadditive manufacturing process in which the part 10 is formed. The asleast one floating structure 28 is encapsulated in, immersed in and/orsurrounded by the powder 12. As illustrated in FIG. 2, the floatingstructures 28 are shown as spherical, however, other shapes such asthree-dimensional ellipses, star shapes, cubes, rectangles, cylinders,polygonal, pyramids, diamonds, triangles and other three-dimensionalgeometries are also possible.

Each of the floating structures 28 are sized so that its largest width34 (or diameter for spherical floating structures 28) is less than thechannel width 36. The floating structures 28 are no mechanically coupledto the internal structure of part 10, so each floating structure 28 maybe easily removed from the part 10 with minimal friction between thefloating structures 28 and the channel walls 16, 18. The floatingstructures 28 may include a depth spacing 32 which defines how far afirst floating structure 28 is behind a second floating structure 28,within the same channel 14. A vertical spacing 30 may define thevertical distance between floating structures 28 within the same channel14. As illustrated in FIG. 2, the floating structures 28 may also bestaggered such that adjacent rows are separated by a vertical stagerdistance 40 and a depth stagger distance 38, where the vertical stagerdistance 40 and the depth stagger distance 38 may be less than therespective vertical spacing 30 and depth spacing 32. In someembodiments, the floating structures 28 may be attached to the part 10using a reduced mechanical coupling or attachment means such that thefloating structures 28 remain in place during the build process but alsoeasily break free due to gravity, vibrations or other forces during thepowder removal process.

During powder removal, the floating structures 28, which are notmechanically coupled to any wall or internal structure of the part 10,are moved back and forth within the channels 14 to push the powder 12out of the channels 14. An external force and/or vibrations may beapplied to the part 10 to cause relative motion between the floatingstructures 28 and the surrounding powder 12, due at least in part to themass and inertia of the floating structures 28. The relative motionbetween the floating structures 28 and the surrounding powder 12 causesthe floating structures to push powder 12 out of the channels 14, whichis also aided by both the external force and/or vibrations, as well asby gravity. The movement of the floating structures 28, which aremechanically decoupled from the part 10, may increase the effectivenessof the powder removal process, compared to a process that uses onlyexternal forces and/or vibrations.

In addition, the floating structures 28 may decrease the magnitude ofthe external forces and/or vibrations required for powder removal, whichmay thus result in reduced stresses on the part 10, and a reducedlikelihood of damaging the part 10 during powder removal processes. Thisprotective aspect may be of particular importance for use with parts 10that are still in a “green,” or non-final processed state during powderremoval. A part structure or “green” state part is a part 10 while it isstill in the process of being manufactured, for example after printingby prior to heat treatment. Furthermore, for parts 10 with complexinternal geometries, such as those including three-dimensionalpassageways and other features that are not readily accessible via anexternal access port, the floating structures 28 within internalinaccessible cavities will aid in powder removal.

The floating structures 28 may be formed via various additivemanufacturing modalities including (but not limited to) powder bed,binder jet, DMLM, DMLS, SLM, EBM and others. Using binder jet and othersimilar modalities, a smooth layer of powder 12 can be spread out acrossa build area and a binder is selectively applied to areas in which apart 10 or floating structure 28 is being formed. Another smoother layerof powder 12 can then be spread out on top and then a successive layerof binder may be selectively applied on top of the first and/or previouslayer according to the desired geometry of the part 10 or floatingstructure 28. The process is repeated over and over again until the part10 or floating structures 28 are formed, one layer at a time. There isno requirement that the part 10 and floating structures 28 be in contactwith each other, and therefore free-floating floating structures 28 canbe formed within the internal cavities of the part 10.

Using other modalities such as but not limited to DMLM, DMLS, SLM, EBMand other modalities that include an external heat source selectivelyapplied to each successive layer of smooth powder, the magnitude of theexternal heat source (e.g., the laser power or electron beam intensity)can be adjusted when forming the first and/or first several layers ofthe floating structures 28, such that the powder 12 may have differentmelt, sintering and/or bonding characteristics. The magnitude of theexternal heat source can then be adjusted, as needed (depending onpowder material properties and the ability to tightly control themagnitude of the heat source), for each successive layer forming thefloating structure 28 allowing floating structures 28 to be formedwithin the internal cavities of the part 10. Such an approach is onemethod of forming a floating structure 28 without a support structure.In addition, it may be possible to use a support structure that isfloating and/or becomes free following the build process to aid inpowder removal, similar to the floating structures 28 described herein.Similar results may also be achievable with DMLM, DMLS, SLM, EBM, etc.via selective application of binders during the build process.

While the application of varying magnitude heat and/or binders duringthe build process described above may be insufficient for providing thedesired material properties of a finished or partially finished part 10,such methodology may be sufficient for use as part of a floatingstructure 28, which may be recycled, scrapped, and/or have no ongoingfunction following the powder removal process. In addition, the exactplacement of a floating structure 28 within a cavity may be lessimportant since the floating structure 28 is intended to move aroundduring the powder removal process. Therefore, if the process describedabove for forming floating structures 28 using DMLM, DMLS, SLM, EBM andother similar modalities produces variations in the location, materialproperties and/or geometry of the floating structure 28, the floatingstructure 28 may nevertheless be sufficient for purposes of powderremoval.

FIG. 3 sectional illustration of a part 10 including a plurality ofcylindrical floating structures 28′ surrounded by powder 12 within thecavities 14. FIG. 3 includes cut surfaces 26 that illustrate the planethrough which a cut was taken, thereby illustrating the internal detailsof the part 10. A vertical spacing 30 and a depth spacing 32 define thevertical and depth-wise distances between the cylindrical floatingstructures 28′. The cylindrical floating structures 28′ are orientedsuch that circular faces 42 face in a depth-wise direction 44. Statedotherwise, the cylinder length of the floating structure 28′ is alignedin the depth-wise direction 44. In other embodiments, the cylindricalfloating structures 28 may be oriented such that circular faces areoriented in a vertical direction 46, or along a width-wise horizontalaxis 48. In other embodiments, multiple floating structures 28′ andvarious combinations along the depth-wise direction 44, verticaldirection 46 and width-wise horizontal axis 48 may be used to enhancethe powder removal process. In addition, the spacings between thecylindrical floating structures 28′ may be defined from sphere center tosphere center in the case of spherical floating structures 28 or fromcircular face 42 to circular face 42 in the case of cylindrical floatingstructures 28′. Other spacing arrangements may be defined as needed.

FIG. 4 illustrates a part 10 including an exemplary single channel 14and an exemplary single floating structure 428. The channel 14 has arectangular cross section with a channel height 50 and a channel width52. The floating structure 428 has a rectangular cross section with afloating structure height 54 and a floating structure width 56. In thearrangement of FIG. 4, the floating structure 428 occupies a highpercentage of the volume of the cavity 14, thereby reducing theavailable volume that powder 12 may occupy. In one embodiment, thefloating structure 428 may occupy form about 60% to about 100% of thevolume of the channel 14. In another embodiment, the floating structure428 may occupy form about 80% to about 99% of the volume of the channel.In another embodiment, the floating structure 428 may occupy form about85% to about 97% of the volume of the channel. In another embodiment,the floating structure 428 may occupy form about 90% to about 95% of thevolume of the channel. In addition, the floating structure 428 has asimilar or identical cross-sectional shape (rectangular in FIG. 4)and/or aspect ratio (the ratio of length to width) which allows thefloating structure corners 58 to be close to the corners 60 of thechannel 14 where powder 12 may be difficult to remove. In oneembodiment, each of the floating structure height 54 and width 56 may begreater than about 80% of the respective channel height 50 and width 52.In another embodiment, each of the floating structure height 54 andwidth 56 may be greater than about 90% of the respective channel height50 and width 52. In another embodiment, each of the floating structureheight 54 and width 56 may be greater than about 95% of the respectivechannel height 50 and width 52. In another embodiment, each of thefloating structure height 54 and width 56 may be greater than about 99%of the respective channel height 50 and width 52. The floating structure428 of FIG. 4 may be designed such that the floating structure 428 canonly be in a single orientation within the channel 14, thereby ensuringthat the floating structure corners 58 will be close to the corners 60of the channel 14.

FIG. 5 illustrates a part 10 including an exemplary single channel 14and an exemplary single floating structure 528. The channel 14 isdefined in part by walls that meet at corners 60. The floating structure528 includes a first planar section 62A and a second planar section 62Bwhich intersect to form an X-shaped cross section. A plurality of corneredges 64 of the x-shaped floating structure 528 of FIG. 5 are orientedclose to the corners 60 of the channel 14 to enhance powder removalwithin the channel 14, while reducing the volume of the floatingstructure 528 when compared to the embodiment of FIG. 4. In otherembodiments, floating structures 528 with other arrangements includingarms and/or portions that are biased toward a corner or internal areawithin a channel 14 may be used to aid in the powder removal process.

FIG. 6 illustrates a part 10 including an exemplary single channel 14and multiple floating structures 28A and 28B. A first floating structure28A may be jack-shaped with 6 prongs 66 extending in 6 mutuallyorthogonal directions. A second floating structure 28B may be spherical.During the powder removal process, the jack-shaped first floatingstructure 28A may be oriented so that at least one of the 6 prongs 66 isproximate one of the corners 60 of the channel 14. The spherical secondfloating structure 28B may aid in pushing the first floating structure28A as well as powder 12 out of the channel 14. Other arrangements usingother combinations and shapes of floating structures 28 are alsopossible.

FIG. 7 illustrates a powder removal process 700 including the steps of:defining a part geometry 702, identifying all of the internal voids 704,identifying the voids needing powder removal 706, defining the minimumdimensions of passageway cross sections 708, defining tolerances 710,defining the shape of a first floating structure 712, defining thedimensions of the first floating structure 714, defining the orientationof the first floating structure 716, defining the placement of the firstfloating structure 718, defining the build characteristics (such asporosity, solidity, fill, hardness, etc.) of the first floatingstructure 720, repeating the above steps for a second through n-numberof floating structures 722, defining the spacings (depth, vertical andhorizontal) between floating structures, repeating the above steps foreach additional passageway 724, creating a build file for the part andfloating structures 726, building the part and floating structures 728,defining vibration characteristics 730, initiating a first vibrationsequence (including a vibration frequency, magnitude, orientation andduration) 732, 734, 736, 738 and 740, initiating a second throughn-number of vibration sequences 742, inspecting the part 744, weighingthe part to assess the amount of powder still remaining in the part 746,using a fan, blower, or vacuum 748, and repeating one or more of thesteps. The method of FIG. 7 may include other steps. In addition, insome embodiments, not all of the steps will be performed. In otherembodiments, the steps will be performed in a different order.

Arrangements of the present embodiments may include using the floatingstructures 28 for other purposes during the build process including (butnot limited to) vibration damping, thermal management, structuralsupport and other purposes. The present embodiments may also includeinserting a floating structure 28 into one or more channels 14 of thepart 10 during the build process, after the build process and/or duringthe powder removal processes, including after some of the powder hasbeen removed, and including re-inserting a floating structure 28 thathas already been removed.

The floating structures 28 of the present embodiments may help to loosenpowder 12 that is tightly packed into internal channels 14 and othercavities of a part 10. Once powder 12 is loosened by the floatingstructures 28, powder 12 may begin to flow out as a result of gravityand/or vibrations. The vibration and/or shaking may be applied alongmultiple axes and/or orientation, as needed based on the geometry of thepart 10. Stated otherwise, it may be beneficial to cause the floatingstructures 28 to have momentum in a multitude or orientations to loosenpowder 12 that may be trapped in the internal channels 14 of the part10, which may have particular orientations. The density and/orvibrational characteristics of the floating structures 28 may bedifferent than those of the powder 12, causing the relative motiontherebetween during the powder removal process. The floating structures28 of the present embodiments may strike a balance between mass,density, structural stiffness, shape and other factors so as to allowthe floating structures 12 to be easily removable from the part 10without damaging the part 10 and while simultaneously yielding efficientpowder 12 removal.

By allowing the floating structures 28 to be filled with loose powder 12during the build process, the floating structures 28 may achieve thedesired mass without needing to be a monolithic solid. In addition,filling the floating structures 28 with loose powder 12 may reduce theamount of binder that is needed during a binder jet build process and/ormay reduce the amount of heat that is required during DMLM, DMLS, SLM,EBM build processes and other similar modalities that include anexternal heat sourced being selectively applied to powder. It may alsobe possible to partially remove loose powder 12 from the interior of afloating structure 28 by blowing or suctioning the powder 12 from thefloating structure 28 while it is partially formed and still has acavity that is open. In such embodiments, the external geometry of thefloating structure 28 is maintained while decreasing the mass of thefloating structure 28 (since it will be hollow or only partially filledwith powder 12), which may be desired to reduces stresses on the part 10during the powder removal process.

The methods and embodiments described herein provide enhanced removal ofpowder from additively manufactured parts, especially parts with complexinternal geometries, those made via powder bed additive manufacturingmodalities, and those with fine feature details. In addition, methodsand embodiments described herein enhance powder removal with additivemodalities such as DMLM, DMLS, SLM, EBM that use a heat source, and alsowith modalities such as binder jet, where the part remains in a greenstate post-printing (prior to heat treatment) during which time the partis structurally less robust and not able to accommodate large vibrationsfrom shaking, which is often used as a means for removing powder.

Although specific features of various embodiments of the presentdisclosure may be shown in some drawings and not in others, this is forconvenience only. In accordance with the principles of embodiments ofthe present disclosure, any feature of a drawing may be referencedand/or claimed in combination with any feature of any other drawing.

This written description uses examples to disclose the embodiments ofthe present disclosure, including the best mode, and also to enable anyperson skilled in the art to practice embodiments of the presentdisclosure, including making and using any devices or systems andperforming any incorporated methods. The patentable scope of theembodiments described herein is defined by the claims, and may includeother examples that occur to those skilled in the art. Such otherexamples are intended to be within the scope of the claims if they havestructural elements that do not differ from the literal language of theclaims, or if they include equivalent structural elements withinsubstantial differences from the literal languages of the claims.

1-11. (canceled)
 12. A powder removal method comprising: identifying apart geometry; identifying at least one cavity within the part to placeat least one powder removal feature; defining at least onecharacteristic of the at least one powder removal feature; creating abuild file for forming the part and the at least one powder removalfeature via a generative build process; generatively forming the partand the at least one powder removal feature; and vibrating the part andthe at least one powder removal feature.
 13. The method of claim 12,wherein defining at least one characteristic of the at least one powderremoval feature comprises at least one of defining a powder removalfeature shape, dimension, orientation within the part, location withinthe part, and porosity.
 14. The method of claim 12, further comprisinggeneratively forming more than one powder removal feature.
 15. Themethod of claim 12, further comprising identifying the dimension of aminimum cross section for the at least one cavity of the part.
 16. Themethod of claim 12, further comprising defining at least one vibrationparameter.
 17. The method of claim 16, further comprising vibrating thepart and the at least one powder removal feature according to the atleast one vibration parameter, wherein the at least one vibrationparameter comprises at least one of a vibration frequency, a vibrationmagnitude, a vibration orientation, and a vibration duration.
 18. Themethod of claim 17, further comprising at least one post-vibrating step,wherein the at least one post-vibrating step comprises at least one ofvisually inspecting the part, weighing the part, air-blowing the part,and vacuuming the part.
 19. The method of claim 19, further comprisinggeneratively forming more than one powder removal feature, whereindefining at least one characteristic of the at least one powder removalfeature comprises at least one of defining a powder removal featureshape, dimension, orientation within the part, location within the part,and porosity.
 20. (canceled)
 21. A method of additively manufacturing apart structure, the method comprising: additively manufacturing a partstructure and a plurality of floating structures disposed within achannel defined by the part structure, wherein the channel comprises anopening sized for removal of the plurality of floating structures fromthe channel, and wherein the channel contains powder surrounding thefloating structures; and removing the plurality of floating structuresand the powder from the channel through the opening at least in part bycausing relative motion between the plurality of floating structures andthe powder; wherein the plurality of floating structures occupy from 80%to 99% of the volume of the channel.
 22. An article of manufacturecomprising: a part structure and a plurality of floating structuresdisposed within a channel defined by the part structure, the partstructure and the plurality of floating structures formed by an additivemanufacturing process; wherein the channel comprises an opening sizedfor removal of the plurality of floating structures from the channel,and wherein the channel contains powder surrounding the floatingstructures; and wherein the plurality of floating structures occupy from80% to 99% of the volume of the channel.
 23. The article of claim 22,wherein the plurality of floating structures are mechanically decoupledfrom the part structure, and wherein the plurality of floatingstructures are formed concurrently with the part structure via theadditive manufacturing process.
 24. The article of claim 22, wherein theplurality of floating structures are monolithic.
 25. The article ofclaim 22, wherein the additive manufacturing process is binder jetting.26. The article of claim 22, wherein the additive manufacturing processis one of direct metal laser melting (DMLM), direct metal lasersintering (DMLS), selective laser melting (SLM) and electron beammelting (EBM).
 27. The article of claim 22, wherein the plurality offloating structures are one of spherical, elliptical, star-shaped,cubic, rectangular, cylindrical, pyramid-shaped, polygonal,diamond-shaped, and triangular.
 28. The article of claim 22, wherein theplurality of floating structures are spaced apart within the channelalong both a depth-wise direction and one of a horizontal direction anda vertical direction.
 29. The article of claim 22, wherein the pluralityof floating structures include at least two adjacent rows of floatingstructures, and wherein each row of the at least two adjacent rows offloating structures is staggered from the adjacent row of floatingstructures.